MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
Date
MAR 2017
Rev Date
Page
6
VIEW LOOKING LH SIDE
STRIKER
PLATE
(LH SHOWN)
STRIKER
PLATE
(LOWER LH SHOWN)
COMPOSITE SHELL
FIGURE 53- 2
53-20-00 - PLATES/SKINS
The fuselage tubular structure is covered with a com-
posite shell. The shell is riveted and bolted to support
angles, formers and brackets. This shell is a non- struc-
tural covering.
The skins, covering tailcone, are an integral part of tail-
cone structure. Repair or replacement of these skins
should be according to AC 43.13- 1( ) Chap. 2, Sect. 3.
The fuselage assembly and tailcone have panels, cov-
ers or doors at various locations to provide access to
interior for inspection or maintenance purposes. (See
Figure 53- 3).
Belly skins are removable to provide access to all com-
ponents and control systems located below floorboard.
See (Figure 53- 3) and following Table for component
location and identification.
-NOTE-
PR 1766-B2 sealant should be used on all fuse-
lage lap joints, where bonded, to provide positive
electrical ground plane for electrical systems.
53-20-00
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